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Performance characteristics at Mach numbers to 2.0 of various types of side inlets mounted on fuselage of proposed supersonic airplane II : inlets utilizing half of a conical spike

机译：安装在超音速飞机II机身上的各种类型侧入口的马赫数为2.0的性能特征：使用一半锥形钉的入口

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Allen, J L; Simon, P C;
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年度 1952
页码 1-54
总页数 54
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Design of top mounted supersonic inlets for a cylindrical fuselage [J] . Saheby Eiman B., Huang Gouping, Hays Anthony Proceedings of the Institution of Mechanical Engineers . 2019,第8期

机译：圆柱形机身顶部安装的超音速进气口的设计
2. Design of top mounted supersonic inlets for a cylindrical fuselage [J] . Saheby Eiman B., Huang Gouping, Hays Anthony Proceedings of the Institution of Mechanical Engineers . 2019,第8期

机译：用于圆柱形机身的顶部安装超音速入口的设计
3. Effects of Mach Number on the Performance of a Diverterless Supersonic Inlet [J] . Askari R., Solani M. R. Journal of Aircraft . 2019,第4期

机译：马赫数对无分流超音速进气口性能的影响
4. The Effects of Fixed Conical Spike Inlets on the Performance of Higher Bypass Ratio Engines [C] . Spencer C. Cleary, Timothy T. Takahashi AIAA aviation technology, integration and operations conference;AIAA aviation forum . 2018

机译：固定圆锥形尖齿进气口对高旁路比发动机性能的影响
5. The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets [D] . Cleary, Spencer. 2018

机译：高旁路比率涡发发动机与固定锥形尖峰入口的超音速性能
6. Withdrawal: Experimental Evaluation of Aerodynamic Performance And Structural Excitation Characteristics of a Supersonic Air Inlet [O] . Doğancan Bahan, M. Tuğrul Akpolat, Özgür Harputlu, 2020

机译：退出：超音速空气入口的空气动力学性能和结构励磁特性的实验评价

Performance characteristics at Mach numbers to 2.0 of various types of side inlets mounted on fuselage of proposed supersonic airplane II : inlets utilizing half of a conical spike

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